Interference of Wing and Fuselage From Tests of the 18 Combinations in the N.A.C.A. Variable-Density Tunnel - Combination With Split Flaps

Author: Sherman, Albert
Year: 1938
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-640
Link: https://digital.library.unt.edu/ark:/67531/metadc54523/

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